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Originated as private venture military transport
based on stillborn An-60 64-73 seat civil airliner designed
to meet 1967 specification. Revised design, following
issue of military requirement in 1968, included relocation
of engines above wings; Two
static test airfriunes; first of four prototype An-72, built at
Kiev, flew (SSSR-197744) 31 August 1977. Production
order placed in December 1980 for improved An-72A
version; manufacture transferred to Kharkov, Ukraine,
where first production An-72 flew 22 December 1985;
An-74 also produced at Kharkov from December 1989.
An-74 announced February 1984; An-72P maritime patrol
version demonstrated 1992. Production of An-74 also
started by Polyot Industrial Association at Omsk, Russia,
in 1993 (assisted by Progress at Arsenyev); first Polyot
aircraft (RA-74050) was flown 25 December 1993.
Development of An-74-200 and An-74TK-200 by
Antonov started 1995; An-74TK certified by Aeronautical
Register (now Interstate Aviation Committee) on 2 August
1991.
| CREW | 2-3 |
| PASSENGERS | 32 |
| ENGINE | 2 x turbo-jet Lotarev D-30, 62.8kN |
| WEIGHTS |
| Take-off weight | 26500-30500 kg | 58423 - 67241 lb |
| DIMENSIONS |
| Wingspan | 25.8 m | 84 ft 8 in |
| Length | 26.6 m | 87 ft 3 in |
| Height | 8.2 m | 26 ft 11 in |
| PERFORMANCE |
| Cruise speed | 720 km/h | 447 mph |
| Ceiling | 11000 m | 36100 ft |
| Range w/max.fuel | 3200 km | 1988 miles |
| Range w/max.payload | 1000 km | 621 miles |
| Shamel, shammilflight(@)yahoo.com, 21.07.2008 Can you provide me the Engine specification and what kind of inspection do you use for this aircraft |
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Do you have any comments about this aircraft ?
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